View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 23097U 94026A 24364.83580665 0.00000000 00000-0 00000-0 0 05
2 23097 62.5827 197.1041 6621079 263.6713 22.9832 2.00604814 06
| Epoch (UTC): | 29 December 2024 20:03:33 |
| Eccentricity: | 0.6621079 |
| inclination: | 62.5827° |
| perigee height: | 2595 km |
| apogee height: | 37761 km |
| right ascension of ascending node: | 197.1041° |
| argument of perigee: | 263.6713° |
| revolutions per day: | 2.00604814 |
| mean anomaly at epoch: | 22.9832° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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